20140615010549A

Accident · Substantial damage

FAA accident report · Piper PA-28-180 · Quincy, CA · June 15, 2014

Date
June 15, 2014 · 11:00 local
Place
Quincy, CA
Airport
Gansner Field
Phase of flight
Takeoff: Rotation
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4931L
NTSB investigation
NTSBWPR14LA249
Reported as
Piper PA-28-180
Reported engine
Lycoming O&VO-360 series
People aboard
4
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
2,397 total1,075 in this make and model21 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On the third flight of the day, the pilot performed a preflight inspection and before takeoff runup. The pilot stated takeoff acceleration was normal with 10 degrees of flaps.

Upon rotation and flap retraction, the pilot noticed a performance degradation. 10 degrees of flaps were again selected; however, altitude could not be maintained even with the engine appearing to develop normal RPM. The pilot decided to perform an emergency landing in a pasture and hit a fence during landing.

Investigation revealed the rear exhaust muffler was approximately 90 % restricted due to internal flame tube failure.

As the FAA filed it

ON THE THIRD FLIGHT OF THE DAY, THE PILOT PERFORMED A PREFLIGHT INSPECTION AND BEFORE TAKEOFF RUNUP. THE PILOT STATED TAKEOFF ACCELERATION WAS NORMAL WITH 10 DEGREES OF FLAPS.

UPON ROTATION AND FLAP RETRACTION, THE PILOT NOTICED A PERFORMANCE DEGRADATION. 10 DEGREES OF FLAPS WERE AGAIN SELECTED; HOWEVER, ALTITUDE COULD NOT BE MAINTAINED EVEN WITH THE ENGINE APPEARING TO DEVELOP NORMAL RPM. THE PILOT DECIDED TO PERFORM AN EMERGENCY LANDING IN A PASTURE AND HIT A FENCE DURING LANDING.

INVESTIGATION REVEALED THE REAR EXHAUST MUFFLER WAS APPROXIMATELY 90 % RESTRICTED DUE TO INTERNAL FLAME TUBE FAILURE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.